Conformal Ablative Thermal Protection Systems (CA-TPS) for Venus and Saturn BackshellsThe new conformal ablator C-PICA, which was developed under STMD GCD, is an optimal candidate for use on the backshells for high velocity entry vehicles at both Venus and Saturn. The material has been tested at heat fluxes up to 400 Wcm2 in shear and over 1800 Wcm2 and 1.5 atm in stagnation with good results. C-PICA has similar density to PICA, but shows half the thermal penetration and similar recession at the same conditions, allowing for a lighter weight TPS to be flown. This poster for VEXAG will show the progress made in the development of the material and why it should be considered for use.
Document ID
20160000590
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Beck, R. (NASA Ames Research Center Moffett Field, CA United States)
Gasch, M. (NASA Ames Research Center Moffett Field, CA United States)
Stackpoole, M. (NASA Ames Research Center Moffett Field, CA United States)
Wilder, M. (NASA Ames Research Center Moffett Field, CA United States)
Boghozian, T. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Chavez-Garcia, J. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Prabhu, D. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Kazemba, C. (Science and Technology Corp. Moffett Field, CA, United States)
Venkatapathy, E. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
January 11, 2016
Publication Date
October 27, 2015
Subject Category
Engineering (General)
Report/Patent Number
ARC-E-DAA-TN27564Report Number: ARC-E-DAA-TN27564
Meeting Information
Meeting: Venus Exploration Analysis Group (VEXAG) Meeting